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52 Cards in this Set
- Front
- Back
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L FUEL PRES LO |
Left side fuel pressure low. |
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CABIN ALT HI |
Cabin altitude exceeds 10,000 feet. |
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CABIN DIFF HI |
Cabin differential is high. |
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R FUEL PRES LO |
Right side fuel pressure low. |
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L OIL PRES LO |
Left engine oil pressure failure. |
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L ENVIR FAIL |
Left environmental air duct overtemp or overpressure. |
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CABIN DOOR |
Cabin door open or not secure. |
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R ENVIR FAIL |
Right environmental air duct overtemp or overpressure. |
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R OIL PRES LO |
Right engine oil pressure failure. |
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L AC BUS |
Left AC bus inoperative inverter. |
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CARGO DOOR |
Cargo door open or not secure. |
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R AC BUS |
Right AC bus inoperative inverter. |
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L BL AIR FAIL |
Left bleed air line failed or melted, or system is off. |
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A/P TRIM FAIL |
Improper trim or no trim from autopilot trim command. |
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ARM EMER LITES |
Emergency light controls are disarmed. |
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A/P FAIL |
Selected APC-65 computer has failed. |
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R BL AIR FAIL |
Right bleed air line failed or melted, or system is off. |
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L DC GEN |
Left generator is off. |
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L FUEL QTY |
Left side fuel quantity is below 324 pounds of usable fuel. |
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STALL HEAT |
Insufficient current to provide heat on stall warning transducer. |
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BATTERYCHARGE |
Excessive charge rate on battery. |
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PROP GND SOL |
One or both ground idle low-pitch-stop solenoids are malfunctioning. |
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R FUEL QTY |
Right side fuel quantity is below 324 pounds of usable fuel. |
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R DC GEN |
Right generator is off. |
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L FW VALVE |
Left fuel firewall valve has not reached its selected position. |
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L COL TANK LOW |
Left fuel system collector tank is below 53 pounds of usable fuel. |
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L GEN TIE OPEN |
Left generator bus is isolated from the center bus. |
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BATT TIE OPEN |
Battery is isolated from the generator buses. |
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R GEN TIE OPEN |
Right generator bus is isolated from the center bus. |
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R COL TANK LOW |
Right fuel system collector tank is below 53 pounds of usable fuel. |
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R FW VALVE |
Right fuel firewall valve has not reached its selected position. |
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L ENG ICE FAIL |
Left ice vane malfunction. Ice vane has not attained the proper position. |
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L BK DI OVHT |
Left brake deice plumbing melted or failed. |
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HYD FLUID LOW |
Landing gear hydraulic fluid level is low. |
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ANTI SKID FAIL |
Electrical failure or low hydraulic oil pressure in the antiskid brake system. |
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ANNPWRSOURCE |
Partial power loss to some annunciator lights. |
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R BK DI OVHT |
Right brake deice plumbing melted or failed. |
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R ENG ICE FAIL |
Right ice vane malfunction. Ice vane has not attained the proper position. |
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L FIRE LOOP |
Left engine fire detection sense loop is open. |
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L PITOT HEAT |
Insufficient current for left pitot heat. |
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XFR VALVE FAIL |
Fuel cross-transfer valve is not fully open or is fully closed for two seconds or more. |
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PWR STEER FAIL |
Electrical failure or low hydraulic oil pressure in power steering system. |
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MAN STEER FAIL |
Nose gear will not free-caster with power steering not engaged. |
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R PITOT HEAT |
Insufficient current for right pitot heat. |
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R FIRE LOOP |
Right engine fire detector sense loop is open. |
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L NO AUX XFR |
No fuel transfer from left auxiliary to main tank. |
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AUTOFEATHER OFF |
Autofeather system is turned off with landing gear extended. |
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PITCH TRIM OFF |
Electric trim disable by switch on the control wheel, while the system is powered on. |
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AFX DISABLE |
Autofeather system is not capable of feathering the propellers. |
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R NO AUX XFR |
No fuel transfer from right auxiliary to main tank. |
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YD/RB FAIL |
The selected FYD-65 computer has failed. |
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RUD BOOST OFF |
Rudder boost system is turned off. |
